NYC89FA129

NTSB accident investigation · Brantly Helicopter B-2 · Herkimer, NY · April 28, 1989

Accident · FatalField investigationFinal report
Date
April 28, 1989, 10:30 local (14:30 UTC)
Place
Herkimer, NY
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N2113UBrantly Helicopter B-2
Weather
Visual (VMC) · Day
Status
Completed · report June 22, 1992
Report
Approved by Office Director
FAA report
19890428010569A
Case key
36284

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

A forced landing in unsuitable terrain due to an internal engine failure. The engine failure sequence was initiated by a failed oil pressure relief spring which had failed in fatigue due to improper plating of the spring. The spring failure caused oil starvation to the engine crankshaft and resulting failure of a connecting rod.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - mech failure/malfCruise - normal
Lubricating system,oil filter/screen - fatigueCause
Maintenance - improperCause
Material defect(inadequate quality of material)Cause
Lubricating system,oil filter/screen - failure,totalCause
Fluid,oil - starvationCause
Engine assembly,crankshaft - overtemperatureCause
Engine assembly,connecting rod - failure,totalCause
Forced landingManeuvering - turn to landing area (emergency)
In flight collision with terrain/waterManeuvering - turn to landing area (emergency)
Terrain condition - none suitableCause
Terrain condition - high obstruction(s)Factor
Object - tree(s)Factor

Analysis

The aircraft was found in a wooded area about 1-1/2 miles north of the departure heliport. On-scene investigation revealed a hole in the engine case near cylinder #4. A later engine teardown showed that the #4 connecting rod had failed at the crankshaft journal. The journal displayed typical discoloration and scoring from overheating and a lack of lubrication. The oil pressure relief valve spring, p/n 68668, was broken into 3 pieces. Metallurgical exam revealed that the spring failed in fatigue which probably originated from pre-existing cracks developed as a result of hydrogen embrittlement. The general condition of the cadmium plating on the spring was very poor, and plating is not called out in the engineering drawing.

Aircraft

Registration
N2113U
Reported as
Brantly Helicopter B-2
Category
Helicopter
Serial number
161
Airframe hours
897
Engine
Lycoming VO 360, 180 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Francis A. Dejohn
Airworthiness certificate
Standard, Normal

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
74
Certificate
Commercial
Airplane ratings
Single-engine sea
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Right
Toxicology
Performed

Weather

Conditions
Visual (VMC) · Day
Lowest ceiling
None

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.